[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3243)
---------------------------------------
Vector Time (GMT): 2012/209/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3768408
20 A = 6781649
56 meter
Y = 4236974
34 meter E =
0005648
Z = -3726359
58 I = 51
29771
XDOT = -2429
355585 Wp = 67
69939
YDOT = -5895
360381 meter/sec RA = 279
87877 deg
ZDOT = -4249
496925 TA = 157
02729
MA = 157
00202
Ha = 219
901 n
mi
Hp = 213
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12363543
96 X = -3797405
12
Y = 13900834
45 feet Y = 4194671
87 meter
Z = -12225589
17 Z = -3744736
29
XDOT = -7970
326724 XDOT = -2342
608909
YDOT = -19341
733532 feet/sec YDOT = -5922
041529 meter/sec
ZDOT = -13941
919046 ZDOT = -4261
088396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17533373
26 X = 5344172
17
Y = -6066455
81 feet Y = -1849055
73 meter
Z = -12301804
11 Z = -3749589
89
XDOT = -3081
143659 XDOT = -939
132587
YDOT = 19442
153294 feet/sec YDOT = 5925
968324 meter/sec
ZDOT = -13989
105004 ZDOT = -4263
879205
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12209
59563290
00016717 00000-0 10270-3 0 9000
2 25544 51
6420 280
4837 0001021 330
3254 29
7841 15
54720176 32448
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
59563290 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 280
4837 deg
Eccentricity:
0001021
Arg of perigee: 330
3254 deg
Mean anomaly: 29
7841 deg
Mean motion: 15
54720176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3244
Checksum: 282
Coasting Arc #2 (Orbit 3259)
---------------------------------------
Vector Time (GMT): 2012/210/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4078388
35 A = 6777633
53 meter
Y = -2482557
73 meter E =
0006332
Z = 4806391
65 I = 51
27953
XDOT = 1396
694254 Wp = 113
89330
YDOT = 7121
713066 meter/sec RA = 274
85865 deg
ZDOT = 2488
180694 TA = 311
51737
MA = 311
57168
Ha = 219
795 n
mi
Hp = 213
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13380539
21 X = 4082497
54
Y = -8144874
44 feet Y = -2436928
20 meter
Z = 15769001
48 Z = 4826213
83
XDOT = 4582
330229 XDOT = 1304
867070
YDOT = 23365
200348 feet/sec YDOT = 7136
818065 meter/sec
ZDOT = 8163
322487 ZDOT = 2494
743440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15559335
73 X = -4742485
53
Y = 831961
55 feet Y = 253581
88 meter
Z = 15850997
72 Z = 4831384
11
XDOT = 7206
936991 XDOT = 2196
674395
YDOT = -21568
491615 feet/sec YDOT = -6574
076244 meter/sec
ZDOT = 8189
653478 ZDOT = 2496
206380
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12210
62406989
00016717 00000-0 10270-3 0 9018
2 25544 51
6413 275
3520 0001074 337
4975 22
6131 15
54739501 32602
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
62406989 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 275
3520 deg
Eccentricity:
0001074
Arg of perigee: 337
4975 deg
Mean anomaly: 22
6131 deg
Mean motion: 15
54739501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3260
Checksum: 284
Coasting Arc #3 (Orbit 3274)
---------------------------------------
Vector Time (GMT): 2012/211/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4234728
62 A = 6775653
39 meter
Y = 455622
89 meter E =
0014496
Z = -5282224
00 I = 51
27216
XDOT = -335
240260 Wp = 82
60590
YDOT = -7641
618468 meter/sec RA = 269
82824 deg
ZDOT = -389
464732 TA = 183
65141
MA = 183
66200
Ha = 219
944 n
mi
Hp = 213
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13893466
59 X = -4213849
24
Y = 1494825
77 feet Y = 408384
87 meter
Z = -17330131
24 Z = -5302745
09
XDOT = -1099
869621 XDOT = -247
873288
YDOT = -25070
926733 feet/sec YDOT = -7644
878793 meter/sec
ZDOT = -1277
771429 ZDOT = -390
881952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12922322
14 X = 3938723
79
Y = 5033332
94 feet Y = 1534159
88 meter
Z = -17414807
40 Z = -5308033
30
XDOT = -10226
711181 XDOT = -3117
101568
YDOT = 21806
768790 feet/sec YDOT = 6646
703127 meter/sec
ZDOT = -1282
839894 ZDOT = -391
009600
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12211
58822181
00016717 00000-0 10270-3 0 9021
2 25544 51
6423 270
5409 0001153 339
4282 20
6825 15
54731103 32751
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
58822181 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 270
5409 deg
Eccentricity:
0001153
Arg of perigee: 339
4282 deg
Mean anomaly: 20
6825 deg
Mean motion: 15
54731103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3275
Checksum: 276
Coasting Arc #4 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2012/212/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213747
93 A = 6776498
00 meter
Y = 1626031
81 meter E =
0005938
Z = 5049371
46 I = 51
27517
XDOT = -744
784714 Wp = 44
58571
YDOT = 7428
494528 meter/sec RA = 264
79625 deg
ZDOT = -1765
217925 TA = 62
59827
MA = 62
53787
Ha = 219
819 n
mi
Hp = 213
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13824632
30 X = 4170723
88
Y = 5334750
02 feet Y = 1672911
45 meter
Z = 16566179
33 Z = 5069736
95
XDOT = -2443
519402 XDOT = -819
221443
YDOT = 24371
701206 feet/sec YDOT = 7419
749872 meter/sec
ZDOT = -5791
397392 ZDOT = -1769
015997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9904485
60 X = -3018887
21
Y = -10894795
42 feet Y = -3320733
64 meter
Z = 16650012
36 Z = 5074923
77
XDOT = 12227
391635 XDOT = 3726
908970
YDOT = -20018
815317 feet/sec YDOT = -6101
734909 meter/sec
ZDOT = -5807
804979 ZDOT = -1770
218957
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12212
61663995
00016717 00000-0 10270-3 0 9033
2 25544 51
6409 265
4091 0001208 349
3592 10
7535 15
54777342 32911
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
61663995 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 265
4091 deg
Eccentricity:
0001208
Arg of perigee: 349
3592 deg
Mean anomaly: 10
7535 deg
Mean motion: 15
54777342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 308
Coasting Arc #5 (Orbit 3305)
---------------------------------------
Vector Time (GMT): 2012/213/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4031998
56 A = 6780006
22 meter
Y = -3516505
45 meter E =
0007404
Z = -4172064
84 I = 51
29133
XDOT = 1832
308936 Wp = 100
62969
YDOT = -6464
907177 meter/sec RA = 259
77167 deg
ZDOT = 3682
521859 TA = 207
36662
MA = 207
40564
Ha = 219
970 n
mi
Hp = 213
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13228341
75 X = -3972110
12
Y = -11537091
37 feet Y = -3561258
53 meter
Z = -13687876
79 Z = -4191506
52
XDOT = 6011
512257 XDOT = 1886
576227
YDOT = -21210
325385 feet/sec YDOT = -6444
114066 meter/sec
ZDOT = 12081
764630 ZDOT = 3691
554162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6898638
72 X = 2102705
08
Y = 16072026
07 feet Y = 4898753
54 meter
Z = -13767724
42 Z = -4196402
40
XDOT = -13316
148277 XDOT = -4058
761995
YDOT = 16085
886025 feet/sec YDOT = 4902
978061 meter/sec
ZDOT = 12119
654681 ZDOT = 3694
070747
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12213
58077423
00016717 00000-0 10270-3 0 9046
2 25544 51
6416 260
5982 0001325 353
4443 6
6693 15
54767885 33062
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
58077423 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 260
5982 deg
Eccentricity:
0001325
Arg of perigee: 353
4443 deg
Mean anomaly: 6
6693 deg
Mean motion: 15
54767885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3306
Checksum: 312
Coasting Arc #6 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2012/214/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3627248
89 A = 6784183
02 meter
Y = 5042384
62 meter E =
0013296
Z = 2714805
61 I = 51
31022
XDOT = -2932
166308 Wp = 95
34958
YDOT = 4885
608084 meter/sec RA = 254
75940 deg
ZDOT = -5136
162311 TA = 53
78109
MA = 53
65824
Ha = 219
962 n
mi
Hp = 213
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11900422
87 X = 3557406
74
Y = 16543256
63 feet Y = 5082556
08 meter
Z = 8906842
57 Z = 2732256
88
XDOT = -9619
968201 XDOT = -2961
630570
YDOT = 16028
897915 feet/sec YDOT = 4852
654380 meter/sec
ZDOT = -16850
926216 ZDOT = -5150
477524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3915904
66 X = -1193567
74
Y = -19967128
50 feet Y = -6085980
77 meter
Z = 8978347
24 Z = 2736600
24
XDOT = 13851
925047 XDOT = 4222
066754
YDOT = -10350
542487 feet/sec YDOT = -3154
845350 meter/sec
ZDOT = -16910
446291 ZDOT = -5154
304029
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12214
60917410
00016717 00000-0 10270-3 0 9050
2 25544 51
6398 255
4657 0001374
4048 359
7105 15
54806462 33220
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
60917410 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 255
4657 deg
Eccentricity:
0001374
Arg of perigee:
4048 deg
Mean anomaly: 359
7105 deg
Mean motion: 15
54806462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 294
Coasting Arc #7 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2012/215/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3003812
92 A = 6786868
38 meter
Y = -6009541
32 meter E =
0010935
Z = -923729
76 I = 51
32880
XDOT = 3967
158805 Wp = 35
30195
YDOT = -2882
637398 meter/sec RA = 249
75977 deg
ZDOT = 5896
916430 TA = 314
65071
MA = 314
73980
Ha = 219
922 n
mi
Hp = 213
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9855029
26 X = -2931902
58
Y = -19716342
90 feet Y = -6042729
71 meter
Z = -3030609
43 Z = -938147
37
XDOT = 13015
612876 XDOT = 3970
453036
YDOT = -9457
471779 feet/sec YDOT = -2838
255997 meter/sec
ZDOT = 19346
838681 ZDOT = 5916
196102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1150086
82 X = 350546
46
Y = 22003920
35 feet Y = 6706794
92 meter
Z = -3089524
54 Z = -941687
08
XDOT = -13994
889050 XDOT = -4265
642182
YDOT = 3439
352183 feet/sec YDOT = 1048
314545 meter/sec
ZDOT = 19426
644528 ZDOT = 5921
241252
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12215
57329054
00016717 00000-0 10270-3 0 9069
2 25544 51
6400 250
6547 0001230 3
5239 356
5922 15
54844976 33376
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
57329054 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 250
6547 deg
Eccentricity:
0001230
Arg of perigee: 3
5239 deg
Mean anomaly: 356
5922 deg
Mean motion: 15
54844976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 299
Coasting Arc #8 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2012/216/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2091594
08 A = 6786910
10 meter
Y = 6370360
55 meter E =
0008772
Z = -1029945
79 I = 51
33862
XDOT = -4883
973772 Wp = 135
10646
YDOT = 659
869242 meter/sec RA = 244
76413 deg
ZDOT = -5873
646014 TA = 56
10558
MA = 56
02217
Ha = 220
059 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6862185
31 X = 2025207
07
Y = 20900133
04 feet Y = 6393378
89 meter
Z = -3379087
25 Z = -1019946
28
XDOT = -16023
535998 XDOT = -4862
457395
YDOT = 2164
925335 feet/sec YDOT = 605
374037 meter/sec
ZDOT = -19270
492172 ZDOT = -5897
319313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1653198
99 X = 503895
05
Y = -21941861
50 feet Y = -6687879
38 meter
Z = -3338416
70 Z = -1017549
41
XDOT = 13920
090171 XDOT = 4242
843484
YDOT = 3977
075371 feet/sec YDOT = 1212
212573 meter/sec
ZDOT = -19368
219240 ZDOT = -5903
433224
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12216
60167222
00016717 00000-0 10270-3 0 9072
2 25544 51
6386 245
5213 0001402 6
9368 353
1804 15
54808674 33538
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
60167222 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 245
5213 deg
Eccentricity:
0001402
Arg of perigee: 6
9368 deg
Mean anomaly: 353
1804 deg
Mean motion: 15
54808674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 294
Coasting Arc #9 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2012/217/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -942589
24 A = 6783884
75 meter
Y = -6091493
18 meter E =
0013821
Z = 2816443
21 I = 51
34239
XDOT = 5563
250430 Wp = 74
55118
YDOT = 1491
193567 meter/sec RA = 239
76514 deg
ZDOT = 5069
885857 TA = 317
60306
MA = 317
70976
Ha = 219
967 n
mi
Hp = 213
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3092484
37 X = -888084
22
Y = -19985213
85 feet Y = -6101729
05 meter
Z = 9240299
26 Z = 2811996
62
XDOT = 18252
133958 XDOT = 5521
534252
YDOT = 4892
367345 feet/sec YDOT = 1553
172027 meter/sec
ZDOT = 16633
483782 ZDOT = 5096
810018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4412093
07 X = -1344805
97
Y = 19744221
51 feet Y = 6018038
72 meter
Z = 9222500
41 Z = 2811018
13
XDOT = -13644
022523 XDOT = -4158
698065
YDOT = -10896
622219 feet/sec YDOT = -3321
290453 meter/sec
ZDOT = 16744
433709 ZDOT = 5103
703394
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12217
63004289
00016717 00000-0 10270-3 0 9080
2 25544 51
6382 240
3889 0001434 4
5462 355
5704 15
54848561 33691
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
63004289 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 240
3889 deg
Eccentricity:
0001434
Arg of perigee: 4
5462 deg
Mean anomaly: 355
5704 deg
Mean motion: 15
54848561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 315
Coasting Arc #10 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2012/218/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -448681
68 A = 6779593
84 meter
Y = 5265375
51 meter E =
0009120
Z = -4256803
68 I = 51
34371
XDOT = -5878
963476 Wp = 61
80442
YDOT = -3380
521238 meter/sec RA = 234
75402 deg
ZDOT = -3563
431015 TA = 171
64395
MA = 171
62875
Ha = 220
075 n
mi
Hp = 213
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1472052
75 X = -486848
59
Y = 17274854
03 feet Y = 5260144
64 meter
Z = -13965891
35 Z = -4259076
06
XDOT = -19287
937912 XDOT = -5823
414786
YDOT = -11090
948943 feet/sec YDOT = -3445
952895 meter/sec
ZDOT = -11691
046636 ZDOT = -3591
855350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7366157
71 X = 2245204
87
Y = -15686053
40 feet Y = -4781109
08 meter
Z = -13975732
24 Z = -4259803
19
XDOT = 12951
469524 XDOT = 3947
607911
YDOT = 16597
811925 feet/sec YDOT = 5059
013075 meter/sec
ZDOT = -11808
026908 ZDOT = -3599
086602
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12218
59413354
00016717 00000-0 10270-3 0 9094
2 25544 51
6378 235
5762 0001537 11
2772 348
8415 15
54833316 33848
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
59413354 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 235
5762 deg
Eccentricity:
0001537
Arg of perigee: 11
2772 deg
Mean anomaly: 348
8415 deg
Mean motion: 15
54833316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3384
Checksum: 316
Coasting Arc #11 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2012/219/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1950772
11 A = 6776115
34 meter
Y = -4007538
67 meter E =
0004563
Z = 5100414
11 I = 51
35055
XDOT = 5751
129298 Wp = 106
34649
YDOT = 4824
084316 meter/sec RA = 229
73214 deg
ZDOT = 1588
320996 TA = 328
26903
MA = 328
29652
Ha = 219
981 n
mi
Hp = 213
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6400170
97 X = 1970663
90
Y = -13148092
75 feet Y = -3985612
67 meter
Z = 16733642
09 Z = 5109939
10
XDOT = 18868
534442 XDOT = 5689
042346
YDOT = 15827
048281 feet/sec YDOT = 4888
049883 meter/sec
ZDOT = 5211
026889 ZDOT = 1616
108536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10339375
15 X = -3151441
54
Y = 10276344
09 feet Y = 3132229
68 meter
Z = 16773293
74 Z = 5112499
93
XDOT = -11693
784488 XDOT = -3564
265512
YDOT = -20470
590363 feet/sec YDOT = -6239
435943 meter/sec
ZDOT = 5325
263689 ZDOT = 1623
140372
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12219
62248655
00016717 00000-0 10270-3 0 9101
2 25544 51
6376 230
4434 0001634 10
8012 349
3175 15
54851242 34002
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
62248655 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 230
4434 deg
Eccentricity:
0001634
Arg of perigee: 10
8012 deg
Mean anomaly: 349
3175 deg
Mean motion: 15
54851242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3400
Checksum: 277
Coasting Arc #12 (Orbit 3414)
---------------------------------------
Vector Time (GMT): 2012/220/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3458066
72 A = 6775355
56 meter
Y = 2506381
69 meter E =
0015115
Z = -5272858
06 I = 51
36877
XDOT = -5069
648001 Wp = 88
63758
YDOT = -5707
619187 meter/sec RA = 224
70452 deg
ZDOT = 613
636988 TA = 187
23851
MA = 187
26036
Ha = 220
099 n
mi
Hp = 213
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11345363
26 X = -3460222
48
Y = 8223037
04 feet Y = 2467699
39 meter
Z = -17299403
09 Z = -5289662
27
XDOT = -16632
703416 XDOT = -5008
428319
YDOT = -18725
784735 feet/sec YDOT = -5763
968845 meter/sec
ZDOT = 2013
244712 ZDOT = 589
157800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13274361
70 X = 4046025
45
Y = -4208971
77 feet Y = -1282894
60 meter
Z = -17368961
71 Z = -5294059
53
XDOT = 9498
103762 XDOT = 2895
022027
YDOT = 22087
558227 feet/sec YDOT = 6732
287748 meter/sec
ZDOT = 1912
724967 ZDOT = 582
998570
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12220
58655837
00016717 00000-0 10270-3 0 9113
2 25544 51
6378 225
6314 0001661 15
7446 344
3758 15
54855119 34157
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
58655837 = yrday
fracday
Element set: 911
Inclination: 51
6378 deg
RA of node: 225
6314 deg
Eccentricity:
0001661
Arg of perigee: 15
7446 deg
Mean anomaly: 344
3758 deg
Mean motion: 15
54855119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3415
Checksum: 314
Coasting Arc #13 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2012/221/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4789384
31 A = 6777589
08 meter
Y = -906947
23 meter E =
0008988
Z = 4704993
74 I = 51
39900
XDOT = 3849
750180 Wp = 54
65137
YDOT = 6041
741611 meter/sec RA = 219
68104 deg
ZDOT = -2745
363619 TA = 62
64494
MA = 62
55349
Ha = 219
932 n
mi
Hp = 213
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15713203
13 X = 4776314
41
Y = -2975548
66 feet Y = -853462
50 meter
Z = 15436331
17 Z = 4728228
41
XDOT = 12630
413978 XDOT = 3795
240306
YDOT = 19821
986914 feet/sec YDOT = 6084
487165 meter/sec
ZDOT = -9007
098486 ZDOT = -2726
794181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15786588
93 X = -4811752
31
Y = -1889559
26 feet Y = -575937
66 meter
Z = 15532293
40 Z = 4734243
03
XDOT = -6232
531712 XDOT = -1899
675666
YDOT = -21578
935233 feet/sec YDOT = -6577
259459 meter/sec
ZDOT = -8930
984673 ZDOT = -2722
164128
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12221
61489170
00016717 00000-0 10270-3 0 9124
2 25544 51
6378 220
4986 0001726 15
0568 345
0636 15
54890859 34316
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
61489170 = yrday
fracday
Element set: 912
Inclination: 51
6378 deg
RA of node: 220
4986 deg
Eccentricity:
0001726
Arg of perigee: 15
0568 deg
Mean anomaly: 345
0636 deg
Mean motion: 15
54890859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 314
Coasting Arc #14 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2012/222/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5773143
16 A = 6781791
74 meter
Y = -587057
17 meter E =
0005937
Z = -3513759
67 I = 51
43727
XDOT = -2136
107865 Wp = 78
93103
YDOT = -5831
254902 meter/sec RA = 214
67035 deg
ZDOT = 4491
474587 TA = 239
58451
MA = 239
64318
Ha = 220
088 n
mi
Hp = 213
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18940758
41 X = -5749080
58
Y = -1926040
60 feet Y = -651481
42 meter
Z = -11528082
92 Z = -3541746
69
XDOT = -7008
227905 XDOT = -2092
561210
YDOT = -19131
413719 feet/sec YDOT = -5854
898819 meter/sec
ZDOT = 14735
809011 ZDOT = 4481
203176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17530142
93 X = 5343187
57
Y = 7244358
85 feet Y = 2208080
58 meter
Z = -11643539
45 Z = -3548950
83
XDOT = 1857
185194 XDOT = 566
070047
YDOT = 19083
242652 feet/sec YDOT = 5816
572360 meter/sec
ZDOT = 14693
914802 ZDOT = 4478
705232
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12222
57894531
00016717 00000-0 10270-3 0 9132
2 25544 51
6379 215
6869 0001811 20
5989 339
5236 15
54883147 34468
Satellite: ISS
Catalog Number: 25544
Epoch time: 12222
57894531 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 215
6869 deg
Eccentricity:
0001811
Arg of perigee: 20
5989 deg
Mean anomaly: 339
5236 deg
Mean motion: 15
54883147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 334
Coasting Arc #15 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2012/223/13:42:54
705
Vector Time (MET): N/A
Weight (LBS) : 908926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6250617
54 A = 6785590
79 meter
Y = 1910051
16 meter E =
0014006
Z = 1802445
96 I = 51
47621
XDOT = 48
170163 Wp = 106
69682
YDOT = 5196
937543 meter/sec RA = 209
67449 deg
ZDOT = -5641
807017 TA = 53
43785
MA = 53
30902
Ha = 220
063 n
mi
Hp = 213
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20507275
41 X = 6220038
60
Y = 6266572
04 feet Y = 1979778
41 meter
Z = 5913536
63 Z = 1832736
72
XDOT = 158
038593 XDOT = 17
459745
YDOT = 17050
320023 feet/sec YDOT = 5197
304703 meter/sec
ZDOT = -18509
865540 ZDOT = -5641
647417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18023857
11 X = -5493671
65
Y = -11552768
68 feet Y = -3521283
89 meter
Z = 6038401
77 Z = 1840504
86
XDOT = 3491
882867 XDOT = 1064
325898
YDOT = -15176
891801 feet/sec YDOT = -4625
916621 meter/sec
ZDOT = -18509
647917 ZDOT = -5641
740685
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12223
60725887
00016717 00000-0 10270-3 0 9145
2 25544 51
6382 210
5538 0001835 21
6018 338
5212 15
54921318 34624
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
60725887 = yrday
fracday
Element set: 914
Inclination: 51
6382 deg
RA of node: 210
5538 deg
Eccentricity:
0001835
Arg of perigee: 21
6018 deg
Mean anomaly: 338
5212 deg
Mean motion: 15
54921318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 293
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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